VOYAGER
Voyager LECP Data Analysis Handbook
Instrument Modeling Reports
by Sheela Shodhan
E.4 FDMOD1.CMN
**************************************************************************
* THIS IS A .CMN FILE THAT IS INCLUDED IN THE ROUTINE FDMOD1.FOR *
* *
* PURPOSE : IT CONTAINS ALL THE PARAMETERS OF TRANSLATION, *
* ROTATION,MAGNETISATION CONSTANTS A0,B0,MAGS THAT ARE *
* USED TO DETERMINE THE MAGNETIC FIELD AT A POINT (X,Y,Z) *
* IN SPACE DUE TO TWO TILTED MAGNETS. *
* VARIABLES : *
* A0,B0 : MAGNETISATION CONSTANTS. *
* ANGLE : ANGLE IN DEGREES BY WHICH THE MAGNETS ARE TILTED. *
* ANG : ANGLE IN RADIANS BY WHICH THE MAGNETS ARE TILTED. *
* HALFD : HALF THE DISTANCE BETWEEN THE MAGNETS. *
* LENGTHS : ARRAY THAT CONTAINS THE LENGTHS OF THE MAGNET PIECES. *
* MAGS : 2-D ARRAY THAT CONTAINS THE MAGNETISATION OF THE MAGNET PIECES.*
* MAX : MAXIMUM NUMBER OF PIECES OF THE MAGNET IN X AND Y DIRECTION. *
* NX1,NY1 : NUMBER OF PIECES OF THE MAGNET IN X AND Y DIRECTION. *
* SEPTS : ARRAY THAT CONTAINS THE DISTANCE BETWEEN THE CORRESPONDING *
* PIECES OF THE TWO MAGNETS. *
* WIDTHS : ARRAY THAT CONTAINS THE WIDTH OF THE MAGNET PIECES. *
* X0,Y0 : CONSTANTS USED IN THE EXPRESSION OF THE LINEARLY FALLING *
* MAGNETISATION : A(X-X0) + B(Y-Y0) *
* XL,YL,ZL : CONSTANTS BY WHICH THE EXPERIMENTAL SYSTEM IS TRANSLATE *
* -D WITH RESPECT TO THE COORDINATE SYSTEMS CENTRED AT THE MAGNETS. *
**************************************************************************
INTEGER MAX,NX1,NY1
REAL*8 HALFD
PARAMETER (HALFD=0.4375D0,MAX=15,NX1=1,NY1=1)
REAL*8 ANGLE,ANG,PI,RAD,A0,B0,X0,Y0
REAL*8 XL(MAX),YL(MAX),ZL(MAX),LENGTHS(MAX),WIDTHS(MAX),SEPTS(MAX)
REAL*8 MAGS(MAX,MAX)
PI = 4.0D0 * DATAN(1.0D0)
RAD = 180.0D0/PI
DATA A0/0.75D0/,B0/3.5D0/,X0/0.0D0/,Y0/0.0D0/
DATA (LENGTHS(I),I=1,NX1)/0.4D0/
DATA (WIDTHS(I),I=1,NY1)/0.3D0/
DATA (XL(I),I=1,NX1)/0.0D0/
DATA (YL(I),I=1,NY1)/0.5D0/
DATA ZL(1)/0.43750D0/
DATA SEPTS(1)/0.8750D0/
DATA ANGLE/20.0D0/
ANG = ANGLE/RAD
YL(1) = 0.5D0 * DCOS(ANG)
DATA (MAGS(1,I),I=1,NY1)/1491.008264378091/
C------------------------------------------------------------------------- C-------------------------------------------------------------------------
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Updated 8/9/19, Cameron Crane
VOYAGER 1 ELAPSED TIME
--:--:--:--
Days: Hours:
Minutes: Seconds
*Since official launch
September 5, 1977, 12:56:00:00 UTC
*Since official launch
September 5, 1977, 12:56:00:00 UTC
VOYAGER 2 ELAPSED TIME
--:--:--:--
Days: Hours:
Minutes: Seconds
*Since official launch
August 20, 1977, 14:29:00:00 UTC
*Since official launch
August 20, 1977, 14:29:00:00 UTC
QUICK FACTS
Manufacturer:
Voyagers 1 and 2 were built in the Jet Propulsion
Laboratory in Southern California.
Mission Duration: 40+ years have elapsed for both Voyager 1 and Voyager 2 (both are ongoing).
Destination: Their original destinations were Saturn and Jupiter. Their current destination is interstellar space.
Mission Duration: 40+ years have elapsed for both Voyager 1 and Voyager 2 (both are ongoing).
Destination: Their original destinations were Saturn and Jupiter. Their current destination is interstellar space.

